ROCKETS TECHNOLOGY

A Numerical Research on Interior Flow for Underwater Launched Missile

  • HOU Jinying ,
  • TAN Dacheng ,
  • BI Shihua
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  • School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

Received date: 2009-06-30

  Online published: 2025-05-28

Abstract

A two-dimensional model of interior flow was constructed for underwater missile concentric canister launcher (CCL). Two-phase flow problem was reduced to a simple high-speed gas jet. The numerical simulation indicates that the results such as the missile's velocity and displacement calculated with single-phase high-speed gas jet model and VOF model are not very different. The single phase high-speed gas jet model can give the flow details in the interior flow for underwater launched missile well and tru-ly. The simulation based on VOF model costs much more time than that based on single-phase high-speed gas jet model. A simple model of the interior flow for underwater launching is feasible.

Cite this article

HOU Jinying , TAN Dacheng , BI Shihua . A Numerical Research on Interior Flow for Underwater Launched Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(3) : 119 -121 . DOI: 10.15892/j.cnki.djzdxb.2010.03.030

References

[1]
戚隆溪, 曹勇, 王柏懿.水下欠膨胀高速气体射流的实验研究[J]. 水力学报, 2000, 32(6): 667-675.
[2]
苗佩云, 袁曾凤.筒内复杂流场三维数值模拟[J]. 弹箭与制导学报, 2004, 24(1): 71-72.
[3]
王福军.计算流体动力学分析[M]. 北京: 清华大学出版社, 2004.
[4]
高娜.导弹水下发射内流场的数值模拟[D]. 哈尔滨: 哈尔滨工程大学, 2006.
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